Transient temperature analysis of airplane carbon composite disk brakes

Ahmet Z. Sahin; Ahmed Z. Al-Garni

Transient temperature analysis of airplane carbon composite disk brakes

King Fahd University of Petroleum and Minerals

Research output: Contribution to conference › Paper › peer-review

Abstract

A numerical transient temperature analysis of a multiple carbon/carbon aircraft disc brake system is obtained using temperature dependent thermo-physical properties. Convective type boundary conditions are used. The maximum temperatures are found to occur around the middle disc and between the mid and outer radiuses of discs.

Original language	English
Publication status	Published - 1997
Externally published	Yes
Event	32nd Thermophysics Conference, 1997 - Atlanta, United States Duration: 23 Jun 1997 → 25 Jun 1997

Conference

Conference	32nd Thermophysics Conference, 1997
Country/Territory	United States
City	Atlanta
Period	23/06/97 → 25/06/97

Bibliographical note

Publisher Copyright:
© 1997 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.

Cite this

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title = "Transient temperature analysis of airplane carbon composite disk brakes",

abstract = "A numerical transient temperature analysis of a multiple carbon/carbon aircraft disc brake system is obtained using temperature dependent thermo-physical properties. Convective type boundary conditions are used. The maximum temperatures are found to occur around the middle disc and between the mid and outer radiuses of discs.",

author = "Sahin, \{Ahmet Z.\} and Al-Garni, \{Ahmed Z.\}",

note = "Publisher Copyright: {\textcopyright} 1997 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.; 32nd Thermophysics Conference, 1997 ; Conference date: 23-06-1997 Through 25-06-1997",

year = "1997",

language = "English",

}

TY - CONF

T1 - Transient temperature analysis of airplane carbon composite disk brakes

AU - Sahin, Ahmet Z.

AU - Al-Garni, Ahmed Z.

PY - 1997

Y1 - 1997

N2 - A numerical transient temperature analysis of a multiple carbon/carbon aircraft disc brake system is obtained using temperature dependent thermo-physical properties. Convective type boundary conditions are used. The maximum temperatures are found to occur around the middle disc and between the mid and outer radiuses of discs.

AB - A numerical transient temperature analysis of a multiple carbon/carbon aircraft disc brake system is obtained using temperature dependent thermo-physical properties. Convective type boundary conditions are used. The maximum temperatures are found to occur around the middle disc and between the mid and outer radiuses of discs.

UR - https://www.scopus.com/pages/publications/84964053059

M3 - Paper

AN - SCOPUS:84964053059

T2 - 32nd Thermophysics Conference, 1997

Y2 - 23 June 1997 through 25 June 1997

ER -

Transient temperature analysis of airplane carbon composite disk brakes

Abstract

Conference

Bibliographical note

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